ES2038918B1 - APPARATUS AND METHOD FOR SEPARATING THE VIBRATION DATA IN A COMMON WAY FROM THE DIGITAL DATA OF THE VIBRATIONS OF THE WINGS OF A TURBINE. - Google Patents

APPARATUS AND METHOD FOR SEPARATING THE VIBRATION DATA IN A COMMON WAY FROM THE DIGITAL DATA OF THE VIBRATIONS OF THE WINGS OF A TURBINE.

Info

Publication number
ES2038918B1
ES2038918B1 ES09102400A ES9102400A ES2038918B1 ES 2038918 B1 ES2038918 B1 ES 2038918B1 ES 09102400 A ES09102400 A ES 09102400A ES 9102400 A ES9102400 A ES 9102400A ES 2038918 B1 ES2038918 B1 ES 2038918B1
Authority
ES
Spain
Prior art keywords
data
circuit
digital data
wings
vibrations
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
ES09102400A
Other languages
Spanish (es)
Other versions
ES2038918A2 (en
ES2038918R (en
Inventor
Michael Twerdochlib
Paul Francis Rozelle
Santitavee Sarasas
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of ES2038918A2 publication Critical patent/ES2038918A2/en
Publication of ES2038918R publication Critical patent/ES2038918R/es
Application granted granted Critical
Publication of ES2038918B1 publication Critical patent/ES2038918B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H11/00—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties
    • G01H11/06—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties by electric means
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/003—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
    • G01H1/006—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines of the rotor of turbo machines

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Turbines (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

APARATO Y METODO PARA SEPARAR LOS DATOS DE VIBRACION DE MODO COMUN DE LOS DATOS DIGITALES DE LAS VIBRACIONES DE LOS ALABES DE UNA TURBINA, DERIVADOS DE UN SENSOR (18); UN PRIMER CIRCUITO (28) ES SENSIBLE AL SENSOR (18) PRODUCIENDO DATOS DIGITALES REPRESENTATIVOS DEL MOMENTO REAL DE LLEGADA DE ALABE (12) AL SENSOR, UN SEGUNDO CIRCUITO (36) ESTABLECE LOS MOMENTOS ESPERADOS DE LLEGADA DE ALABE (12) AL SENSOR (18), UN TERCER CIRCUITO (38) ES SENSIBLE A LOS DATOS DIGITALES GENERANDO UNA PLURALIDAD DE ENTRADAS DE DATOS QUE REPRESENTAN LA DIFERENCIA ENTRE EL MOMENTO REAL Y EL MOMENTO ESPERADO, UN CUARTO CIRCUITO (40, 46) ALMACENA LAS ENTRADAS DE DATOS EN UNA PRIMERA SECUENCIA (42) CON UNA PLURALIDAD DE ENTRADAS FIGURADAS AL PRINCIPIO (D1-D50) Y AL FINAL (D51-D100) E INTERCALA EN LA SECUENCIA (42) CARACTERES DE RESERVA DE ESPACIO SI NO SE PRODUCE LA ENTRADA DE DATOS PARA UN ALABE (12), Y UN QUINTO CIRCUITO (52, 54) ESTABLECE UN VALOR DE PROMEDIO DINAMICO DE ENTRADAS DE DATOS.APPARATUS AND METHOD FOR SEPARATING THE VIBRATION DATA IN A COMMON WAY FROM THE DIGITAL DATA OF THE VIBRATIONS OF THE WINGS OF A TURBINE, DERIVED FROM A SENSOR (18); A FIRST CIRCUIT (28) IS SENSITIVE TO THE SENSOR (18) PRODUCING DIGITAL DATA REPRESENTATIVE OF THE REAL TIME OF ARRIVAL OF ALABE (12) TO THE SENSOR, A SECOND CIRCUIT (36) ESTABLISHES THE EXPECTED TIMES OF ARRIVAL OF ALABE (12) 18), A THIRD CIRCUIT (38) IS SENSITIVE TO DIGITAL DATA, GENERATING A PLURALITY OF DATA ENTRIES THAT REPRESENT THE DIFFERENCE BETWEEN THE REAL TIME AND THE EXPECTED TIME, A FOURTH CIRCUIT (40, 46) STORES THE DATA ENTRIES IN A FIRST SEQUENCE (42) WITH A PLURALITY OF FIGURE INPUTS AT THE BEGINNING (D1-D50) AND AT THE END (D51-D100) AND INTERCALATE IN SEQUENCE (42) SPACE RESERVATION CHARACTERS IF NO DATA ENTRY IS PRODUCED FOR AN ALABE (12), AND A FIFTH CIRCUIT (52, 54) ESTABLISHES A DYNAMIC AVERAGE VALUE OF DATA ENTRIES.

ES09102400A 1990-11-01 1991-10-30 APPARATUS AND METHOD FOR SEPARATING THE VIBRATION DATA IN A COMMON WAY FROM THE DIGITAL DATA OF THE VIBRATIONS OF THE WINGS OF A TURBINE. Expired - Lifetime ES2038918B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/607,934 US5148711A (en) 1990-11-01 1990-11-01 Apparatus and method for removing common mode vibration data from digital turbine blade vibration data

Publications (3)

Publication Number Publication Date
ES2038918A2 ES2038918A2 (en) 1993-08-01
ES2038918R ES2038918R (en) 1994-07-01
ES2038918B1 true ES2038918B1 (en) 1995-01-16

Family

ID=24434312

Family Applications (1)

Application Number Title Priority Date Filing Date
ES09102400A Expired - Lifetime ES2038918B1 (en) 1990-11-01 1991-10-30 APPARATUS AND METHOD FOR SEPARATING THE VIBRATION DATA IN A COMMON WAY FROM THE DIGITAL DATA OF THE VIBRATIONS OF THE WINGS OF A TURBINE.

Country Status (6)

Country Link
US (1) US5148711A (en)
JP (1) JP3095270B2 (en)
KR (1) KR100195652B1 (en)
CA (1) CA2054598C (en)
ES (1) ES2038918B1 (en)
IT (1) IT1251959B (en)

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US5471880A (en) * 1994-04-28 1995-12-05 Electric Power Research Institute Method and apparatus for isolating and identifying periodic Doppler signals in a turbine
US5761956A (en) * 1995-10-17 1998-06-09 Westinghouse Electric Corporation Passive combustion turbine blade vibration monitor sensor
GB9618096D0 (en) * 1996-08-29 1996-10-09 Rolls Royce Plc Identification of resonant frequencies of vibration of rotating blades
US6094989A (en) * 1998-08-21 2000-08-01 Siemens Westinghouse Power Corporation Method and apparatus for analyzing non-synchronous blade vibrations using unevenly spaced probes
US6346807B1 (en) * 1999-10-22 2002-02-12 Bently Nevada Corporation Digital eddy current proximity system: apparatus and method
JP3530474B2 (en) 2000-09-22 2004-05-24 三菱重工業株式会社 Wing vibration measurement method and wing vibration monitoring system using the same
FR2840358B1 (en) * 2002-05-28 2006-09-15 Snecma Moteurs METHOD AND SYSTEM FOR DETECTING ROTOR DAMAGE OF AN AIRCRAFT ENGINE
KR100505929B1 (en) * 2003-03-31 2005-08-04 삼성광주전자 주식회사 A compressor and A method for connecting pipeline of compressor
US7348683B2 (en) * 2005-11-17 2008-03-25 General Electric Company Rotor for a wind energy turbine
US7824147B2 (en) * 2006-05-16 2010-11-02 United Technologies Corporation Airfoil prognosis for turbine engines
DE102006060650A1 (en) * 2006-12-21 2008-06-26 Mtu Aero Engines Gmbh Device and method for contactless blade vibration measurement
US7861592B2 (en) * 2007-02-27 2011-01-04 Siemens Energy, Inc. Blade shroud vibration monitor
US7987725B2 (en) * 2007-09-21 2011-08-02 Siemens Energy, Inc. Method of matching sensors in a multi-probe turbine blade vibration monitor
GB0811073D0 (en) * 2008-06-18 2008-07-23 Rolls Royce Plc Timing analysis
US7866213B2 (en) * 2008-06-18 2011-01-11 Siemens Energy, Inc. Method of analyzing non-synchronous vibrations using a dispersed array multi-probe machine
GB0822859D0 (en) * 2008-12-16 2009-01-21 Rolls Royce Plc Timing analysis
US9045999B2 (en) * 2010-05-28 2015-06-02 General Electric Company Blade monitoring system
US9512736B2 (en) 2012-05-14 2016-12-06 United Technologies Corporation Monitoring one or more turbine engine rotor blades by correlating measurement data and reference data as a function of time
US20150081229A1 (en) * 2013-09-16 2015-03-19 General Electric Company Compressor blade monitoring system
EP3071940B1 (en) 2013-11-18 2019-01-30 United Technologies Corporation Monitoring a dynamic parameter such as torque in a rotational system
JP6455702B2 (en) * 2014-08-22 2019-01-23 株式会社Ihi Method and apparatus for measuring vibration of rotating body
US11193388B2 (en) * 2018-11-27 2021-12-07 General Electric Company Methods and systems for monitoring rotor blades in turbine engines
CN113340244B (en) * 2021-03-04 2023-06-13 北京化工大学 Non-contact turbine mechanical blade vibration displacement monitoring method and device
KR102522543B1 (en) * 2021-03-09 2023-04-14 두산에너빌리티 주식회사 Automatic diagnosis device and method for blade
CN113530617B (en) * 2021-05-18 2022-06-21 西安交通大学 Method for extracting natural frequency difference between blades based on blade end timing sensor

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4049644A (en) * 1976-06-23 1977-09-20 Wennerstrom Arthur J Device for measuring tip deflection of rotating blades
GB8318509D0 (en) * 1983-07-08 1983-08-10 Rolls Royce Vibration monitoring in rotary blade machines
US4573358A (en) * 1984-10-22 1986-03-04 Westinghouse Electric Corp. Turbine blade vibration detection apparatus
US4790189A (en) * 1987-03-02 1988-12-13 Westinghouse Electric Corp. Method for eliminating sensor drift in a vibration monitoring system
US4887468A (en) * 1988-06-03 1989-12-19 Westinghouse Electic Corp. Nonsynchronous turbine blade vibration monitoring system
US4922757A (en) * 1988-06-13 1990-05-08 Westinghouse Electric Corp. Apparatus for precise detection of blade passing times in a steam turbine
US5015949A (en) * 1988-12-22 1991-05-14 Westinghouse Electric Corp. Steam turbine blade arrival time processor with automatic gain control
US4996880A (en) * 1989-03-23 1991-03-05 Electric Power Research Institute, Inc. Operating turbine resonant blade monitor

Also Published As

Publication number Publication date
JPH04362206A (en) 1992-12-15
CA2054598A1 (en) 1992-05-02
KR920010271A (en) 1992-06-26
IT1251959B (en) 1995-05-27
CA2054598C (en) 2002-10-08
ITMI912768A0 (en) 1991-10-18
JP3095270B2 (en) 2000-10-03
KR100195652B1 (en) 1999-06-15
US5148711A (en) 1992-09-22
ES2038918A2 (en) 1993-08-01
ES2038918R (en) 1994-07-01
ITMI912768A1 (en) 1993-04-18

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